EP3878752C0 - Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé - Google Patents

Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé

Info

Publication number
EP3878752C0
EP3878752C0 EP19883087.9A EP19883087A EP3878752C0 EP 3878752 C0 EP3878752 C0 EP 3878752C0 EP 19883087 A EP19883087 A EP 19883087A EP 3878752 C0 EP3878752 C0 EP 3878752C0
Authority
EP
European Patent Office
Prior art keywords
control method
propulsion system
hybrid electric
method therefor
electric propulsion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP19883087.9A
Other languages
German (de)
English (en)
Other versions
EP3878752B1 (fr
EP3878752A1 (fr
EP3878752A4 (fr
Inventor
Chang Mo Moon
Ji Ho Moon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Changinaviation Co Ltd
Changinaviation Co Ltd
Original Assignee
Changinaviation Co Ltd
Changinaviation Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from KR1020180136057A external-priority patent/KR102004227B1/ko
Priority claimed from KR1020190084226A external-priority patent/KR102279741B1/ko
Application filed by Changinaviation Co Ltd, Changinaviation Co Ltd filed Critical Changinaviation Co Ltd
Publication of EP3878752A1 publication Critical patent/EP3878752A1/fr
Publication of EP3878752A4 publication Critical patent/EP3878752A4/fr
Application granted granted Critical
Publication of EP3878752B1 publication Critical patent/EP3878752B1/fr
Publication of EP3878752C0 publication Critical patent/EP3878752C0/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0083—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by several motors of different type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/16—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants
    • B64D31/18—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants for hybrid-electric power plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Mechanical Engineering (AREA)
  • Hybrid Electric Vehicles (AREA)
  • Automation & Control Theory (AREA)
EP19883087.9A 2018-11-07 2019-10-29 Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé Active EP3878752B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
KR1020180136057A KR102004227B1 (ko) 2018-11-07 2018-11-07 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기 및 그 제어 방법
KR1020190084226A KR102279741B1 (ko) 2019-07-12 2019-07-12 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기 및 그 제어 방법
PCT/KR2019/014336 WO2020096254A1 (fr) 2018-11-07 2019-10-29 Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé

Publications (4)

Publication Number Publication Date
EP3878752A1 EP3878752A1 (fr) 2021-09-15
EP3878752A4 EP3878752A4 (fr) 2022-07-06
EP3878752B1 EP3878752B1 (fr) 2024-04-17
EP3878752C0 true EP3878752C0 (fr) 2024-04-17

Family

ID=70612135

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19883087.9A Active EP3878752B1 (fr) 2018-11-07 2019-10-29 Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé

Country Status (4)

Country Link
US (1) US20210387723A1 (fr)
EP (1) EP3878752B1 (fr)
CN (1) CN113056422B (fr)
WO (1) WO2020096254A1 (fr)

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KR101970601B1 (ko) * 2019-03-13 2019-04-19 문창모 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기
EP4143085A4 (fr) * 2020-04-30 2024-04-24 Volansi, Inc. Aéronef à décollage et atterrissage verticaux (vtol) fixe hybride alimenté par un moteur à combustible lourd
CN112429248A (zh) * 2020-12-01 2021-03-02 飞的科技有限公司 飞行器
CN112373684A (zh) * 2020-12-01 2021-02-19 飞的科技有限公司 飞行器及其驱动系统
CN112429249A (zh) * 2020-12-01 2021-03-02 飞的科技有限公司 飞行器
CN112429247A (zh) * 2020-12-01 2021-03-02 飞的科技有限公司 飞行器
FR3128200B1 (fr) * 2021-10-20 2024-06-21 Zipair Dispositif volant hybride
DE102021133301B3 (de) * 2021-12-15 2022-11-03 Head Gmbh VTOL-Luftfahrzeug mit batterieelektrischem Antrieb und Verbrennungsmotor
CN118679095A (zh) * 2022-01-14 2024-09-20 弗得哥航空有限公司 带有涡扇发动机核心的并联混合动力装置
US11745890B1 (en) * 2022-04-29 2023-09-05 Beta Air, Llc Fuel pod for hybrid electric aircraft
CN115562040B (zh) * 2022-11-03 2024-06-14 清华大学 一种垂直起降固定翼飞机电推进系统优化设计方法

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DE102009004239A1 (de) 2009-01-05 2010-07-08 Ivan Novikov-Kopp Verfahren zur komplexen Erhöhung von Aerodynamik- und Transporteigenschaften, Bodeneffektfahrzeug zur Ausführung des Verfahrens (Varianten) und Flugverfahren
US20130134264A1 (en) * 2011-11-28 2013-05-30 Carter Aviation Technologies, Llc Electric Motor Powered Rotor Drive for Slowed Rotor Winged Aircraft
US9102326B2 (en) * 2012-03-05 2015-08-11 Embry-Riddle Aeronautical University, Inc. Hybrid assembly for an aircraft
IL222053A (en) * 2012-09-23 2016-11-30 Israel Aerospace Ind Ltd A device, method, and computerized product for aircraft management
DE102013109392A1 (de) * 2013-08-29 2015-03-05 Airbus Defence and Space GmbH Schnellfliegendes, senkrechtstartfähiges Fluggerät
US9246425B2 (en) * 2014-04-29 2016-01-26 Gulfstream Aerospace Corporation Apparatus and systems for engine and generator control within an aircraft
US11485488B1 (en) * 2014-12-07 2022-11-01 L3Harris Latitude Llc Vertical take-off and landing aircraft with rotor thrust yaw control
CN104843181B (zh) * 2015-04-10 2017-10-20 桂林航龙科讯电子技术有限公司 一种油电混合动力固定翼垂直起降无人机系统
KR101638964B1 (ko) 2015-07-17 2016-07-13 주식회사 한국카본 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기
KR101667330B1 (ko) 2015-07-17 2016-10-19 주식회사 한국카본 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기
KR101615486B1 (ko) * 2015-07-17 2016-04-26 주식회사 한국카본 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기
US10205415B2 (en) * 2015-12-14 2019-02-12 Rolls-Royce North American Technologies Inc. Multiple generator synchronous electrical power distribution system
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KR101970601B1 (ko) * 2019-03-13 2019-04-19 문창모 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기

Also Published As

Publication number Publication date
US20210387723A1 (en) 2021-12-16
EP3878752B1 (fr) 2024-04-17
CN113056422B (zh) 2024-05-14
CN113056422A (zh) 2021-06-29
EP3878752A1 (fr) 2021-09-15
EP3878752A4 (fr) 2022-07-06
WO2020096254A1 (fr) 2020-05-14

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